|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|인용정보||피인용 횟수 : 17 인용 특허 : 10|
A vertical takeoff and landing aircraft, which includes pivotal wing and engine assemblies on a fuselage with tail assemblies extending from each of the wing assemblies and the engines being operable in turbo prop or pure jet mode, wherein the aircraft is configured such that it can be landed or taken off vertically or in a horizontal mode along a runway.
1. A vertical takeoff and landing aircraft comprising:a fuselage for carrying passengers and/or cargo, a tail assembly at the rear end of the fuselage,a movable wing assembly including a wing pivotally mounted at each side of the fuselage and positionable between substantially horizontal and substantially vertical positions for respectively conditioning the aircraft for horizontal and vertical flight modes,an engine carried by each wing assembly, each said engine having a propeller with blades,flaps at the trailing edges of the wings movable between an i...